EP2599719A4 - Flugzeuge mit einer integralen aerodynamischen konfiguration - Google Patents

Flugzeuge mit einer integralen aerodynamischen konfiguration Download PDF

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Publication number
EP2599719A4
EP2599719A4 EP11820241.5A EP11820241A EP2599719A4 EP 2599719 A4 EP2599719 A4 EP 2599719A4 EP 11820241 A EP11820241 A EP 11820241A EP 2599719 A4 EP2599719 A4 EP 2599719A4
Authority
EP
European Patent Office
Prior art keywords
aircraft
aerodynamic configuration
integral aerodynamic
integral
configuration
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP11820241.5A
Other languages
English (en)
French (fr)
Other versions
EP2599719A1 (de
Inventor
Mihail Aslanovich Pogosyan
Aleksandr Nikolaevich Davidenko
Mihail Yurievich Strelets
Vladimir Aleksandrovich Runishev
Aleksey Zaharovich Tarasov
Aleksey Kirillovich Shokurov
Sergey Yurievich Bibikov
Leonid Evgenievich Krylov
Pavel Borisovich Moskalev
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Otkrytoe Akcionernoe Obschestvo Aviacionnaya Holdingovaya Kompaniya Suhoi
Original Assignee
Otkrytoe Akcionernoe Obschestvo Aviacionnaya Holdingovaya Kompaniya Suhoi
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Otkrytoe Akcionernoe Obschestvo Aviacionnaya Holdingovaya Kompaniya Suhoi filed Critical Otkrytoe Akcionernoe Obschestvo Aviacionnaya Holdingovaya Kompaniya Suhoi
Publication of EP2599719A1 publication Critical patent/EP2599719A1/de
Publication of EP2599719A4 publication Critical patent/EP2599719A4/de
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
EP11820241.5A 2010-07-28 2011-04-07 Flugzeuge mit einer integralen aerodynamischen konfiguration Withdrawn EP2599719A4 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2010131640/11A RU2440916C1 (ru) 2010-07-28 2010-07-28 Самолет интегральной аэродинамической компоновки
PCT/RU2011/000229 WO2012026846A1 (ru) 2010-07-28 2011-04-07 Самолет интегральной аэродинамической компоновки

Publications (2)

Publication Number Publication Date
EP2599719A1 EP2599719A1 (de) 2013-06-05
EP2599719A4 true EP2599719A4 (de) 2017-11-15

Family

ID=45723663

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11820241.5A Withdrawn EP2599719A4 (de) 2010-07-28 2011-04-07 Flugzeuge mit einer integralen aerodynamischen konfiguration

Country Status (8)

Country Link
US (1) US9180974B2 (de)
EP (1) EP2599719A4 (de)
CN (1) CN103209892B (de)
EA (1) EA021280B1 (de)
IL (1) IL224415A (de)
RU (1) RU2440916C1 (de)
UA (1) UA106677C2 (de)
WO (1) WO2012026846A1 (de)

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RU2472956C2 (ru) * 2011-04-29 2013-01-20 Открытое акционерное общество "ОКБ Сухого" Сверхзвуковой регулируемый воздухозаборник
GB201312593D0 (en) * 2013-07-13 2013-08-28 Mbda Uk Ltd A thrust flow powered vehicle
CN103538716B (zh) * 2013-08-21 2016-09-07 林仕华 一种高效且稳定的斜形逆变机翼
CN105015795A (zh) * 2014-04-28 2015-11-04 张焰 飞机设计方法与方案
RU2583824C2 (ru) * 2014-08-01 2016-05-10 Открытое акционерное общество "Авиационная холдинговая компания" Сухой" Сверхзвуковой самолет с внутрифюзеляжными грузовыми отсеками
CN104608917A (zh) * 2015-01-28 2015-05-13 梧州晟裕科技有限公司 一种固定翼无人飞行器的尾翼结构
US10000274B2 (en) * 2015-08-20 2018-06-19 The Boeing Company Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft
CN105523189B (zh) * 2015-12-14 2017-11-21 成都飞机设计研究所 一种滑动变体可调caret进气道
CN106167089A (zh) * 2016-07-19 2016-11-30 深圳市创翼睿翔天空科技有限公司 尾翼结构及具有其的无人机
CN106516086A (zh) * 2016-10-19 2017-03-22 戈晓宁 高隐身无平尾升力体布局飞机
RU2632550C1 (ru) * 2016-10-28 2017-10-05 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Летательный аппарат
CN107284641B (zh) * 2017-07-03 2023-09-08 安徽国援智能科技有限公司 一种适于超音速飞行的小型飞机气动外形
US20190185127A1 (en) * 2017-12-18 2019-06-20 Freedom Aircraft Ventures Llc Aircraft design and technology
US11059569B1 (en) * 2017-12-29 2021-07-13 United States Of America As Represented By The Administrator Of Nasa Flight control system for aircraft having multi-functional flight control surface
JP7076156B2 (ja) * 2018-03-29 2022-05-27 国立研究開発法人宇宙航空研究開発機構 超音速機の機体形状の設計方法、超音速機の生産方法
CN108910057B (zh) * 2018-06-10 2024-03-29 东莞理工学院 一种具有多发动机的飞翼无人机
US11167836B2 (en) 2018-06-21 2021-11-09 Sierra Nevada Corporation Devices and methods to attach composite core to a surrounding structure
US11247776B2 (en) * 2019-04-01 2022-02-15 The Boeing Company Aircraft having embedded engines
CN110816870B (zh) * 2019-09-30 2021-03-16 中国科学院力学研究所 一种改善宽域飞行器配平特性的设计方法
DE102020004273B4 (de) * 2020-02-26 2024-07-18 Airbus Defence and Space GmbH Luftfahrzeugstruktur mit einer Einlassöffnung für Triebwerksluft
WO2021251807A1 (ru) * 2020-06-11 2021-12-16 Алдан Асанович САПАРГАЛИЕВ Тяговые поверхности аппарата самоперемещения
RU2749175C1 (ru) * 2020-07-10 2021-06-07 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Самолет интегральной аэродинамической компоновки
CN112298578B (zh) * 2020-11-27 2021-07-27 成都云鼎智控科技有限公司 无人飞行器发动机的控制系统
CN117087865B (zh) * 2023-10-20 2024-01-26 中国空气动力研究与发展中心计算空气动力研究所 一种飞翼气动飞行器及控制方法

Citations (3)

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Publication number Priority date Publication date Assignee Title
GB1029106A (en) * 1965-02-19 1966-05-11 Rolls Royce Aircraft
RU2140376C1 (ru) * 1997-12-10 1999-10-27 АООТ "ОКБ Сухого" Самолет интегральной аэродинамической компоновки
US20050045764A1 (en) * 2003-08-29 2005-03-03 Supersonic Aerospace International, Llc Canard position and dihedral for boom reduction and pitch/directional control

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FR1552118A (de) * 1967-11-17 1969-01-03
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US4025007A (en) * 1974-08-16 1977-05-24 Herbert Kaniut Shifting horizontal tail with helical motions
US4456204A (en) * 1981-09-29 1984-06-26 The Boeing Company Deployable inlet for aeroplane center boost engine
FR2635075B1 (fr) * 1988-08-04 1994-09-23 Onera (Off Nat Aerospatiale) Entree d'air supersonique bidimensionnelle et asymetrique pour l'air de combustion d'un moteur d'aeronef
FR2710607B1 (fr) * 1993-10-01 1995-12-01 Onera (Off Nat Aerospatiale) Entrée d'air supersonique et hypersonique bidimensionnelle, à trois rampes mobiles, pour l'air de combustion d'un moteur d'aéronef .
US5957405A (en) * 1997-07-21 1999-09-28 Williams International Co., L.L.C. Twin engine aircraft
US7520123B2 (en) * 2005-05-12 2009-04-21 Lockheed Martin Corporation Mixing-enhancement inserts for pulse detonation chambers
CN201362361Y (zh) * 2008-12-25 2009-12-16 李振荣 前后攻击型战斗机

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1029106A (en) * 1965-02-19 1966-05-11 Rolls Royce Aircraft
RU2140376C1 (ru) * 1997-12-10 1999-10-27 АООТ "ОКБ Сухого" Самолет интегральной аэродинамической компоновки
US20050045764A1 (en) * 2003-08-29 2005-03-03 Supersonic Aerospace International, Llc Canard position and dihedral for boom reduction and pitch/directional control

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
CARLO KOPP ET AL: "Assessing the Sukhoi PAK-FA Sukhoi/KnAAPO T-50/I-21/Article 701 PAK-FA Air Power Australia Analysis 2010-01 15th February 2010 Assessing the Sukhoi PAK-FA / Sukhoi/KnAAPO T-50/I-21/Article", 15 February 2010 (2010-02-15), XP055412672, Retrieved from the Internet <URL:http://www.ausairpower.net/APA-2010-01.html> [retrieved on 20171004] *
CARLO KOPP ET AL: "Assessing the Sukhoi PAK-FA", 15 February 2010 (2010-02-15), pages 1 - 41, XP055412643, Retrieved from the Internet <URL:https://web.archive.org/web/20100218135042/http://www.ausairpower.net/APA-2010-01.html> [retrieved on 20171004] *
See also references of WO2012026846A1 *

Also Published As

Publication number Publication date
CN103209892B (zh) 2015-09-16
RU2440916C1 (ru) 2012-01-27
US20140145027A1 (en) 2014-05-29
EP2599719A1 (de) 2013-06-05
IL224415A (en) 2017-12-31
EA021280B1 (ru) 2015-05-29
WO2012026846A1 (ru) 2012-03-01
CN103209892A (zh) 2013-07-17
UA106677C2 (uk) 2014-09-25
US9180974B2 (en) 2015-11-10
EA201300030A1 (ru) 2013-05-30

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